US1791857A - Aerial display apparatus - Google Patents

Description

Feb. 10, 1931. 4 Q WERNER 1,791,857

AERIAL DI S PLAY APPARATUS Filed Feb. 19, 1950 ososnwnnnnn, OF SOUTH BElfl'D, INDIANA, ASSIGNQR TO RAINBOW LONG ISLAND crTY, NEW YonK, A coaronsrronos new YORK trio, 7 or Annrat DISPLAY erresarus Application filed February 19, 1930. serial-no. 429,709..-

This invention relates to aerial displays for advertising and similar purposes, and is concerned more particularly with display apparatus which includes electric discharge tubes-such as neon tubes.

' Airplanes havingelectric' discharge tubes "attached to the under surface of the lower any oarticular hindjof airplane.

wing, have beenused heretofore-to some extent for advertising purposes, the tubes being shaped to form letters or other symbols which convey the advertising message. Since these tubes are delicate and fragile, diiliculties have been encountered in attaching the-tubes to the airplane wings' in' such way that the tubes-are afforded the desired degree of protection and the 'aero-dynaniic performance of the Wing surfaces is not interfered With.

The object of this invention is to provide an aerial display apparatus including luIni- I nous discharge tubes and means for'attaching V thein imposition on an airplane wing in such fashion that they can readily be removed and replaced to alter the advertising message and when in place are protected against injrir. This apparatus is so constructed that the tube mounting may be permanently attached in position on the wing and the presence of the *nionntin does not interfereivith the 3erthe airplane and adus onlyan fornian'ce of significant weightthereto.

F or a better nnders ending of the inven-' ion, reference may be had to the accompanydra ings, in which r Fig. 1 is a bottom plan of an airplane with the apparatus of the invention in under the Wing surface;

Fig. 2 is a partial end view; 3 is a sectional view in perspective on the line 3-3 of Fig. 1; and

4 is a sectional end view of the parts illustrated in Fig. 3. i V i In these drawings, the apparatus is shown installed on the under surface of the wing of a 'inonoplaneof the three-motor type. It will be understood that this'airplaneis shown position merely forv purposes of illustration and that the utility of the invention is not limited to Monntedon the under surface of each wing desired, are stringers l0,eachfstringer preferably being. niaoe in the form of a channel I} ll of aluminum or other light mateof that sort; These stringers are placed i with theirleng'ths' parallel to thei'direction flight and each stringer issecured to" the under surface of the wingstrncture in' any' convenient manner, for instance, by U-shaped supports 12. V Preferably the supports "are attached to the- W1n surface in such a"vva'* that the attaching means, which may-be but the stringers on eachfwing are all mounted" :o-that their lower surfaceslie in a plane accordingly the length of the supports 2 by which'a stringeris-attached to thawing will vary. A lso, each'= snp'port is of "suit: cient length so that the stringer. to which it is attached lies at a substantial distance from} theiii der surface of-the win so thatlthe r r 7 2D? p 7 n contact with the stringer, the tube, being secured tothe stringer by binding wires 17. The rubber rings'perniit the tubes to securely held in position and at'thetiine cushion them against shock. v I The stringers lie in v I stringrsrelatively closely. spaced so "that" theyprovidepa suitableineans of support for For example, eachftube may be providedw th split-rubber rings 1'6 surroundthe tube and lying ness froni the fuselafg e toward the t ip, f

andthus change its hero-dynamic ajro-w with adj acent" tubesof different sizes andshlaiaes; =Where the'tubesare bent to form letters; the spacing" of the stringers and the size ofxthe letters Will] preferably, be .co-ordinatedso that all parts a'n-d on the under surface of the fuselage, if '0 stringer. For example, the letter I can be secured to a single stringer, while the letter 1)will have its upright bar attached to one stringer and the'remainder extending across and attached-to two adjacent stringers. The letter L may be mounted either on two or three stringers, the upright portion extending lengthwiseof one stringer and the lateral bar extending across the next stringerand if desired to the second adjacent stringer to be attached thereto. The letters M. and W may occupy four stringers. By thus corree lating the spacing of the stringers and the size of the letters, the letters maybe changed and the proper spacingbetween letters, so necessary for good readability, may be obtained without changing the relative position of the stringers.

The mounting means for the tubes can be permanentlyattached to the wings of the air plane and by reason of the light weight of the parts, their low head resistance and their spacing wing from the surface, their presence does not affect the performance of the plane. When the plane is to be used for-display purposes, tubes in the form of letters spelling out the words ofthe message or in the form of symbols, such, for example, as a trade-mark, may be readily attached in place. When the message is to be changed,

the tubes are removed and others substituted for them. This replacement of the tubes in-' volvesno changein the stringers or' their supports and the tubes can be 7 quickly and safely secured in position throughout the display surface. As the stringers all form one plane, it is merely necessary that the tubing forming the letters be flat, a condition which is easily met by ordinary manufacturing methods. Similar stringers may also be placed at the bottom of the fuselage to permit luminous tubes to be mounted thereon. These stringers may be ofwoo-d or of metal.

I claim Q1. The combination: with a wing of an air- V plurality of supports mounted on plane of a the under surface of the wing, these supports being of a plurality of members mounted on said supports, said members being of sheet metal and extending parallel and edgewise to the direction of flight,'and luminous tubes attached to said members; 7

V 2. The combination of an airplane, a plurality ofU-shaped brackets the legs of which are connected to said airplane, a'plurality bfparallel channel-shaped members. lying in the direction of flight andattachedto said ttshaped brackets'in such a manner that the bottom of the U of each of. the U-sha ped brackets is in the channel of afchannel memher, and luminous tubes supported on said channel members. a V 3. The combination-of an airplane, a plurality of U-shaped brackets the legs of which are connected to said airplane, a. plurality of parallel channel-shaped members lying in the direction of flight and attached to said U-shaped brackets so that the bottom of the U of the brackets is in the channel of a channel member, and luminous tubes supported on said channel members, at least some of the parallel to the direction of flight, each member being completely separate and having separate means forpermanently supporting it from the airplane, luminous; tubes forming a, design to be displayed and means for removabl-y fastening said tubes to said-elongatedmembers, at least some of said tubes being attached to a plurality of elongated members,- said tubes having each of their ends adjacent and supported upon one of said parallel members.

6. The combination with a wing of an airplane of a plurality'of sheet metal brackets mounted on the under surface of the wing landlying with their edges in the direction of flight, a plurality of channel-shaped; mem

bers lying in the direction of flight and attached to said brackets and luminous tubes supported on said channel members.

series of parallel elongated imembers'lying Ull In testimony whereof I affix my signature.

osoan WERNER.

sheet metal and lying with their edges opposed to the direction of flight,

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